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A Comparative Study of Airfoil Stall Characteristics Based on Detached Eddy Simulation Incorporated with Weighted Essentially Non-Oscillatory Scheme and Weighted Compact Nonlinear Scheme

In this paper, the detached eddy simulation (DES) method is used to calculate the aerodynamic characteristics of NACA0015 airfoil by combining the Riemann approximate solution HLLC (Harten–Lax–van Leer Contact) with the high-order weighted essentially non-oscillatory (WENO) scheme and the weighted c...

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Principais autores: Yan Qi, Bowen Zhong, Song Zou
Formato: Artigo
Idioma:Inglês
Publicado em: MDPI AG 2024-11-01
coleção:Aerospace
Assuntos:
detached eddy simulation
WENO scheme
WCNS
numerical dissipation
Acesso em linha:https://www.mdpi.com/2226-4310/11/11/917
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